View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39439U 13066Z 23333.81650335 .00017431 00000-0 16142-2 0 9991
2 39439 97.7015 295.2197 0054909 86.5270 274.2228 14.93399829542004
| Epoch (UTC): | 29 November 2023 19:35:45 |
| Eccentricity: | 0.0054909 |
| inclination: | 97.7015° |
| perigee height: | 549 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 295.2197° |
| argument of perigee: | 86.5270° |
| revolutions per day: | 14.93399829 |
| mean anomaly at epoch: | 274.2228° |
| orbit number at epoch: | 54200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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